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Design requirements and development of an airborne descent path definition algorithm for time navigationThe design requirements for a 4D path definition algorithm are described. These requirements were developed for the NASA ATOPS as an extension of the Local Flow Management/Profile Descent algorithm. They specify the processing flow, functional and data architectures, and system input requirements, and recommended the addition of a broad path revision (reinitialization) function capability. The document also summarizes algorithm design enhancements and the implementation status of the algorithm on an in-house PDP-11/70 computer. Finally, the requirements for the pilot-computer interfaces, the lateral path processor, and guidance and steering function are described.
Document ID
19860019467
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Izumi, K. H.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Thompson, J. L.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Groce, J. L.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Schwab, R. W.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:178037
NASA-CR-178037
Report Number: NAS 1.26:178037
Report Number: NASA-CR-178037
Accession Number
86N28939
Funding Number(s)
PROJECT: RTOP 505-45-33-11
CONTRACT_GRANT: NAS1-16300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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